CA1004477A - Diverter valve for a gas turbine with an augmenter - Google Patents
Diverter valve for a gas turbine with an augmenterInfo
- Publication number
- CA1004477A CA1004477A CA205,261A CA205261A CA1004477A CA 1004477 A CA1004477 A CA 1004477A CA 205261 A CA205261 A CA 205261A CA 1004477 A CA1004477 A CA 1004477A
- Authority
- CA
- Canada
- Prior art keywords
- augmenter
- gas turbine
- diverter valve
- diverter
- valve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
- F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings for the reversed flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/877—With flow control means for branched passages
- Y10T137/87788—With valve or movable deflector at junction
- Y10T137/87812—Pivoted valve or deflector
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00417954A US3837411A (en) | 1973-11-21 | 1973-11-21 | Diverter valve for a gas turbine with an augmenter |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1004477A true CA1004477A (en) | 1977-02-01 |
Family
ID=23656036
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA205,261A Expired CA1004477A (en) | 1973-11-21 | 1974-07-22 | Diverter valve for a gas turbine with an augmenter |
Country Status (2)
Country | Link |
---|---|
US (1) | US3837411A (en) |
CA (1) | CA1004477A (en) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3943707A (en) * | 1974-10-23 | 1976-03-16 | General Electric Company | Gas turbine engine exhaust nozzle diverter valve |
US4000612A (en) * | 1975-07-28 | 1977-01-04 | General Electric Company | Cooling system for a thrust vectoring gas turbine engine exhaust system |
DE2540537C2 (en) * | 1975-09-11 | 1977-11-10 | Motoren- und Turbinen-Union München GmbH, 8000 München | Gas turbine jet engine for propelling and controlling an aircraft |
US4000854A (en) * | 1975-10-02 | 1977-01-04 | General Electric Company | Thrust vectorable exhaust nozzle |
US4529130A (en) * | 1982-04-26 | 1985-07-16 | Rolls-Royce Inc. | Turbo machine nozzle with thrust reverser |
GB2254589B (en) * | 1983-12-20 | 1993-04-14 | British Aerospace | Jet propulsion powerplants |
US4605169A (en) * | 1983-12-27 | 1986-08-12 | United Technologies Corporation | Exhaust nozzle construction |
US4753392A (en) * | 1984-11-02 | 1988-06-28 | United Technologies Corporation | Two dimensional gas turbine engine exhaust nozzle |
US4790495A (en) * | 1984-12-06 | 1988-12-13 | Grumman Aerospace Corporation | Cascade thrust reverser |
US4742961A (en) * | 1987-05-04 | 1988-05-10 | United Technologies Corporation | Exhaust gas nozzle including a cooling air diverter |
US4848081A (en) * | 1988-05-31 | 1989-07-18 | United Technologies Corporation | Cooling means for augmentor liner |
US4922711A (en) * | 1988-06-10 | 1990-05-08 | The Boeing Company | Thrust reversing system for high bypass fan engines |
DE3831062A1 (en) * | 1988-09-13 | 1990-03-15 | Stober & Morlock | DEVICE BEHIND A GAS TURBINE |
US5244014A (en) * | 1989-05-23 | 1993-09-14 | Henry Ehrenberg | Multi-way valve |
US5039171A (en) * | 1989-08-18 | 1991-08-13 | Societe Anonyme Dite Hispano-Suiza | Multi-panel thrust reverser door |
FR2651021B1 (en) * | 1989-08-18 | 1994-05-06 | Hispano Suiza Sa | TURBOREACTOR DRIVE INVERTER, WITH DOORS ASSOCIATED WITH AN UPSTREAM PANEL |
GB9127505D0 (en) * | 1991-03-11 | 2013-12-25 | Gen Electric | Multi-hole film cooled afterburner combustor liner |
NL9101782A (en) * | 1991-10-24 | 1993-05-17 | Philip Rijk Koudijs | EXHAUST SYSTEM FOR COMBUSTION GASES. |
DE4433759C1 (en) * | 1994-09-22 | 1996-02-08 | Mtu Muenchen Gmbh | Jet engine with thrust reverser |
US5706650A (en) * | 1995-08-09 | 1998-01-13 | United Technologies Corporation | Vectoring nozzle using injected high pressure air |
US5987880A (en) * | 1997-07-08 | 1999-11-23 | Mcdonnell Douglas Corporation | Supersonic engine, multi-port thrust reversing system |
US6938408B2 (en) * | 2001-04-26 | 2005-09-06 | Propulsion Vectoring, L.P. | Thrust vectoring and variable exhaust area for jet engine nozzle |
FR2834533B1 (en) * | 2002-01-10 | 2004-10-29 | Hurel Hispano Le Havre | DEVICE FOR COOLING THE COMMON NOZZLE ON A NACELLE |
US7871242B2 (en) * | 2007-05-31 | 2011-01-18 | United Technologies Corporation | Single actuator controlled rotational flow balance system |
US9157394B2 (en) | 2012-08-15 | 2015-10-13 | United Technologies Corporation | Adjustable cable for exhaust duct liner hanger |
US20160305370A1 (en) * | 2015-04-16 | 2016-10-20 | Honeywell International Inc. | Translating cowl thrust reverser with door pivots aft of reverse flow path |
CN104896514A (en) * | 2015-05-13 | 2015-09-09 | 广东电网有限责任公司电力科学研究院 | Anti-vibration heat insulation wall of main combustion chamber of gas turbine |
US20170058828A1 (en) * | 2015-08-26 | 2017-03-02 | Rohr, Inc. | Cascade with varying vane trailing edge thickness |
US10563614B2 (en) * | 2016-08-17 | 2020-02-18 | Honeywell International Inc. | Composite translating cowl assembly for a thrust reverser system |
US11046445B2 (en) | 2017-07-26 | 2021-06-29 | Raytheon Technologies Corporation | Nacelle |
US10767596B2 (en) * | 2017-07-26 | 2020-09-08 | Raytheon Technologies Corporation | Nacelle |
US11891026B1 (en) * | 2023-05-16 | 2024-02-06 | King Faisal University | Reverse thrust braking system |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2964905A (en) * | 1960-12-20 | Aircraft control means | ||
GB1033583A (en) * | 1965-03-17 | 1966-06-22 | Rolls Royce | Thrust reverser for a jet propulsion engine |
BE755612A (en) * | 1969-06-18 | 1971-02-15 | Gen Electric | PROPULSION TUBES WITH IMPROVED NOISE CANCELLATION SYSTEM |
US3614037A (en) * | 1969-09-22 | 1971-10-19 | Boeing Co | Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser |
DE1964976C3 (en) * | 1969-12-24 | 1973-01-04 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Thrust reverser for a turbine jet engine of an aircraft |
US3690561A (en) * | 1970-11-05 | 1972-09-12 | Rohr Corp | Thrust controlling system |
US3690562A (en) * | 1971-06-23 | 1972-09-12 | Gen Motors Corp | Jet propulsion nozzle |
-
1973
- 1973-11-21 US US00417954A patent/US3837411A/en not_active Expired - Lifetime
-
1974
- 1974-07-22 CA CA205,261A patent/CA1004477A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3837411A (en) | 1974-09-24 |
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